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FR3082229B1 - TURBOMACHINE WITH A PARTIAL COMPRESSION VANE - Google Patents

TURBOMACHINE WITH A PARTIAL COMPRESSION VANE Download PDF

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Publication number
FR3082229B1
FR3082229B1 FR1855007A FR1855007A FR3082229B1 FR 3082229 B1 FR3082229 B1 FR 3082229B1 FR 1855007 A FR1855007 A FR 1855007A FR 1855007 A FR1855007 A FR 1855007A FR 3082229 B1 FR3082229 B1 FR 3082229B1
Authority
FR
France
Prior art keywords
annular
vein
primary
turbomachine
row
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1855007A
Other languages
French (fr)
Other versions
FR3082229A1 (en
Inventor
Ambroise Maxime Victor Retiveau Pierre-Hugues
Claude Cochon Sebastien
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1855007A priority Critical patent/FR3082229B1/en
Publication of FR3082229A1 publication Critical patent/FR3082229A1/en
Application granted granted Critical
Publication of FR3082229B1 publication Critical patent/FR3082229B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/324—Blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/321—Application in turbines in gas turbines for a special turbine stage
    • F05D2220/3216—Application in turbines in gas turbines for a special turbine stage for a special compressor stage
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/321—Application in turbines in gas turbines for a special turbine stage
    • F05D2220/3216—Application in turbines in gas turbines for a special turbine stage for a special compressor stage
    • F05D2220/3217—Application in turbines in gas turbines for a special turbine stage for a special compressor stage for the first stage of a compressor or a low pressure compressor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'invention concerne une turbomachine (1) double flux comprenant : - une soufflante (3) générant un flux d'air et comprenant une rangée annulaire d'aubes de soufflante (13) portées par un rotor (14) d'axe longitudinal X, - un bec de séparation (10), en aval de la rangée d'aubes de soufflante, séparant le flux d'air en un flux primaire circulant dans une veine primaire (6) annulaire et en un flux secondaire circulant dans une veine secondaire (7) annulaire, et - au moins un compresseur (9) agencé en aval d'une entrée de la veine primaire. Selon l'invention, la turbomachine comprend une rangée annulaire d'aubes partielles (20) mobiles s'étendant sensiblement radialement depuis le rotor et étant agencée axialement entre la rangée annulaire ou la dernière des rangées annulaires d'aubes de soufflante et l'entrée de la veine primaire, chaque aube partielle présentant une hauteur inférieure ou égale au moins à une hauteur de l'entrée de la veine primaire.The invention relates to a double flow turbomachine (1) comprising: - a fan (3) generating an air flow and comprising an annular row of fan blades (13) carried by a rotor (14) of longitudinal axis X , - a separation nozzle (10), downstream of the row of fan blades, separating the air flow into a primary flow circulating in a primary annular vein (6) and into a secondary flow circulating in a secondary vein (7) annular, and - at least one compressor (9) arranged downstream of an inlet of the primary vein. According to the invention, the turbomachine comprises an annular row of movable partial blades (20) extending substantially radially from the rotor and being arranged axially between the annular row or the last of the annular rows of fan blades and the inlet of the primary vein, each partial blade having a height less than or equal at least to a height of the entry of the primary vein.

FR1855007A 2018-06-08 2018-06-08 TURBOMACHINE WITH A PARTIAL COMPRESSION VANE Active FR3082229B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1855007A FR3082229B1 (en) 2018-06-08 2018-06-08 TURBOMACHINE WITH A PARTIAL COMPRESSION VANE

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1855007A FR3082229B1 (en) 2018-06-08 2018-06-08 TURBOMACHINE WITH A PARTIAL COMPRESSION VANE
FR1855007 2018-06-08

Publications (2)

Publication Number Publication Date
FR3082229A1 FR3082229A1 (en) 2019-12-13
FR3082229B1 true FR3082229B1 (en) 2020-07-03

Family

ID=62875032

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1855007A Active FR3082229B1 (en) 2018-06-08 2018-06-08 TURBOMACHINE WITH A PARTIAL COMPRESSION VANE

Country Status (1)

Country Link
FR (1) FR3082229B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3112809B1 (en) * 2020-07-23 2022-07-29 Safran Aircraft Engines TURBOMACHINE MODULE EQUIPPED WITH A PROPELLER AND STATOR VANE SUPPORTED BY HOLDING MEANS AND CORRESPONDING TURBOMACHINE

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6561761B1 (en) * 2000-02-18 2003-05-13 General Electric Company Fluted compressor flowpath
US7476086B2 (en) * 2005-04-07 2009-01-13 General Electric Company Tip cambered swept blade
FR2893993B1 (en) * 2005-11-30 2008-01-18 Snecma Sa METHOD FOR REDUCING THE NOISE OF A TURBOMACHINE BLOWER, SILENT DEVICE FOR CARRYING OUT SAID METHOD, BLOWER VANE AND BLOWER COMPRISING SUCH A SILENT DEVICE, AND TURBOMACHINE COMPRISING THE SAME
FR2911923B1 (en) * 2007-01-25 2011-07-08 Snecma ACOUSTIC RECTIFIER FOR TURBOREACTOR BLOWER CASING
FR3027053B1 (en) * 2014-10-10 2019-09-13 Safran Aircraft Engines AIRCRAFT TURBOMACHINE STATOR

Also Published As

Publication number Publication date
FR3082229A1 (en) 2019-12-13

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